Cessna 172S Nav III Quick setup guide

Cessna

172SNAV

SKYHAWK

Information

Manual

172SIMAUS

Model

172S

Nav

III

Avionics

Serials

172S9810and

CESSNA

INTRODUCTION

MODEL

172SNAV

III

NOTICE

THE

TIME

ISSUANCE,

THIS

INFORMATION

MANUAL

WAS

EXACT

DUPLICATE

THE

OFFICIAL

PILOT'S

OPERATING

HANDBOOK

AND

FAA

APPROVED

AIRPLANE

FLIGHT

MANUAL AND

USED

FOR

GENERAL

PURPOSES

ONLY.

WILL

NOT

KEPT

CURRENT

AND,

THEREFORE,

CANNOT

USED

SUBSTITUTE

FOR

THE

OFFICIAL

PILOTS

OPERATING

HANDBOOK

AND

FAA

APPROVED

AIRPLANE

FLIGHT

MANUAL

INTENDED

FOR

OPERATION

THE

AIRPLANE.

THE

PILOT'S

OPERATING

HANDBOOK

MUST

CARRIED

THE

AIRPLANE

AND

AVAILABLE

THE

PILOT

ALL

TIMES.

Cessna

Aircraft

Company

Original

Issue

February

2005

Revision

3-12

October

2006

Revision

U.S.

INTRODUCTION

CESSNA

—

MODEL

172SNAV

III

PERFORMANCE

SPECIFICATIONS

*SPEED:

—

Maximum

Sea

Level

126

KNOTS

Cruise,

75%

Power

8500

Feet

124

KNOTS

i—

CRUISE:

Recommended

lean

mixture

with

fuel

allowance

for

engine

start,

taxi,

takeoff,

climb

and

minutes

reserve.

75%

Power

8500

Feet

Range

518

„

Gallons

Usable

Fuel

Time

4.26

HOURS

Range

10,000

Feet,

45%

Power

Range

638

Gallons

Usable

Fuel

Time

6.72

HOURS

RATE-OF-CLIMB

SEA

LEVEL

730

FPM

SERVICE

CEILING

14,000

FEET

TAKEOFF

PERFORMANCE:

Ground

Roll

960

FEET

Total

Distance

Over

Foot

Obstacle

1630

FEET

LANDING

PERFORMANCE:

—

Ground

Roll

575

FEET

Total

Distance

Over

Foot Obstacle

1335

FEET

STALL

SPEED:

Flaps

Up,

Power

Off

KCAS

Flaps

Down,

Power

Off

KCAS

MAXIMUM

WEIGHT:

—

Ramp

2558

POUNDS

Takeoff

2550

POUNDS

Landing

2550

POUNDS

—

(Continued

Page)

—

U.S.

Revision

—

CESSNA

INTRODUCTION

MODEL

172SNAV

III

PERFORMANCE

SPECIFICATIONS

(Continued)

STANDARD

EMPTY

WEIGHT

1663

POUNDS

MAXIMUM

USEFUL LOAD

895

POUNDS

BAGGAGE

ALLOWANCE

120

POUNDS

WING

LOADING:

Lbs/Sq.

14.7

POWER

LOADING:

Lbs/HP

14.2

FUEL

CAPACITY

GALLONS

OIL

CAPACITY

QUARTS

ENGINE:

Textron

Lycoming

IO-360-L2A

180BHPat2700RPM

PROPELLER:

Fixed

Pitch,

Diameter

INCHES

NOTE

*Speed

performance

shown

for

airplane

equipped

with

speed

fairings

which

increase

the

speeds

approximately

knots.

There

corresponding

difference

range,

while

all

other

performance

figures

are

unchanged

when

speed

fairings

are

installed.

The

above

performance

figures

are

based

airplane

weights

2550

pounds,

standard

atmospheric

conditions,

level,

hard-surfaced

dry

runways

and

wind.

They

are

calculated

values

derived

from

flight

tests

conducted

Cessna

Aircraft

Company

under

carefully

documented

conditions

and

will

vary

with

individual

airplanes

and

numerous

factors

affecting

flight

performance.

Revision

U.S.

iii/iv

CESSNA

INTRODUCTION

MODEL

172SNAVII1

Cessna

Tejttron

Company

Information

Manual

SK^H/WVK

Member

□(

GAMA

Cessna

Aircraft

Company

Model

172S

NAV

III

AVIONICS

OPTION

Serials

172S9810and

THIS

MANUAL

INCORPORATES

INFORMATION

ISSUED

THE

PILOT'S

OPERATING

HANDBOOK

AND

FAA

APPROVED

AIRPLANE

FLIGHT

MANUAL

REVISION

DATED

OCTOBER

2006

(PART

NUMBER

172SPHAUS-04).

CESSNA

AIRCRAFT

COMPANY

WICHITA,

KANSAS USA

172SIMAUS-03

Revision

U.S.

v/vi

CESSNA

INTRODUCTION

MODEL

172SNAV

III

TABLE

CONTENTS

SECTION

GENERAL

LIMITATIONS

EMERGENCY

PROCEDURES

NORMAL

PROCEDURES

PERFORMANCE

WEIGHT

AND

BALANCE/EQUIPMENT

LIST

AIRPLANE

AND

SYSTEMS

DESCRIPTION

HANDLING,

SERVICE

AND

MAINTENANCE

SUPPLEMENTS

Revision

U.S.

vii/viii

CESSNA

SECTION

MODEL

172S

NAV

III

GENERAL

TABLE

CONTENTS

Page

Three

View

Normal

Ground

Attitude

1-3

Introduction 1-5

Descriptive

Data

1-5

Engine

1-5

Propeller

1-5

Fuel

1-5

Oil

1-6

Maximum

Certificated

Weights

1-7

Standard

Airplane

Weights

1-8

Cabin

And

Entry

Dimensions

1-8

Baggage

Space

And

Entry

Dimensions

1-8

Specific

Loadings

1-8

Symbols,

Abbreviations

and

Terminology

1-9

General

Airspeed

Terminology

And

Symbols

1-9

Meteorological

Terminology

1-10

Engine

Power

Terminology

1-10

Airplane

Performance

And

Flight

Planning

Terminology

. .

1-11

Weight

And

Balance

Terminology

1-12

Metric

Imperial

U.S.

Conversion

Charts

1-14

Weight

Conversions

1-15

Length

Conversions

1-17

Distance

Conversions

1-21

Volume

Conversions

1-22

Temperature

Conversions

1-25

Hectopascals

Inches

Mercury

1-26

Volume

Weight

Conversions

1-27

Quick

Conversions

1-28

172SPHAUS-00

U.S.

1-1/1-2

CESSNA

MODEL

172SNAV

SECTION

GENERAL

Figure

1-1.

Three

View

Normal

Ground

Attitude

(Sheet

of 2)

172SPHAUS-00

U.S.

1-3

SECTION

GENERAL

CESSNA

MODEL

172SNAV

III

NOTE

•

Wing

span

shown

with

strobe

lights

installed.

•

Wheel

base

length

65".

•

Propeller

ground

clearance

1/4".

•

Wing

area

174

square

feet.

•

Minimum

turning

radius

pivot

point

outboard

wing

tip)

27'-5

1/2".

•

Normal

ground

attitude

shown

with

nose

strut

showing

approximately

strut,

and

wings

level.

Figure

1-1,

Three

View

Normal

Ground

Attitude

(Sheet

1-4

U.S.

172SPHAUS-00

CESSNA

SECTION

MODEL

172S

NAV

III

GENERAL

INTRODUCTION

This

handbook

contains

sections,

and

includes

the

material

required

furnished

the

pilot

FAR

Part

23.

also

contains

supplemental

data

supplied

Cessna

Aircraft

Company.

Section

provides

basic

data

and

information

general

interest.

also

contains

definitions

explanations

symbols,

abbreviations,

and

terminology

commonly

used.

DESCRIPTIVE

DATA

ENGINE

Number

Engines:

Engine

Manufacturer:

Textron

Lycoming.

Engine

Model

Number:

IO-360-L2A.

Engine

Type:

Normally

aspirated,

direct

drive,

air-cooled,

horizontally

opposed,

fuel

injected,

four

cylinder

engine

with

360

cu.

in.

displacement.

Horsepower

Rating

and

Engine

Speed: 180

rated

BHP

2700

RPM.

PROPELLER

Propeller

Manufacturer:

McCauley

Propeller

Systems.

—

Propeller

Model

Number:

1A170E/JHA7660.

Number

Blades:

Propeller

Diameter:

inches.

Propeller

Type:

Fixed

pitch.

—

FUEL

WARNING

USE

UNAPPROVED

FUELS

MAY

RESULT

DAMAGE

THE

ENGINE

AND

FUEL

SYSTEM

COMPONENTS,

RESULTING

POSSIBLE

ENGINE

FAILURE.

—'

Approved

Fuel

Grades

(and

Colors):

100LL

Grade

Aviation

Fuel

(Blue).

100

Grade

Aviation

Fuel

(Green).

(Continued

Page)

172SPHAUS-00

U.S.

1-5

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